3 edition of Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport found in the catalog.
Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport
by National Aeronautics and Space Administration, Langley Research Center, Available from NASA Center for AeroSpace Information, National Technical Information Service [distributor in Hampton, Va, Hanover, MD, Springfield, VA
Written in English
|Statement||David E. Hahne, Louis J. Glaab.|
|Series||NASA/TP ; 1999-209539, NASA technical paper -- 209539.|
|Contributions||Glaab, Louis J., Langley Research Center.|
|The Physical Object|
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